Unsteady aerodynamic analysis of space shuttle vehicles. Part 1: Summary report [PDF]
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show that slender wing theory can be modified to give the potential flow static and dynamic characteristics over a large Mach number range from M = 0 to M 1. A
Ericsson, L. E., Reding, J. P.
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Unsteady transonic flow calculations for two-dimensional canard-wing configurations with aeroelastic applications [PDF]
Unsteady transonic flow calculations for aerodynamically interfering airfoil configurations are performed as a first step toward solving the three dimensional canard wing interaction problem.
Batina, J. T.
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Fully unsteady subsonic and supersonic potential aerodynamics for complex aircraft configurations for flutter applications [PDF]
A general theory for study, oscillatory or fully unsteady potential compressible aerodynamics around complex configurations is presented. Using the finite-element method to discretize the space problem, one obtains a set of differential-delay equations ...
Morino, L., Tseng, K.
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Unsteady viscous vortex with flow toward the center [PDF]
Strong unsteady viscous vortex of annular region, with tangential and radial flow, and core region with uniform axial flow toward ...
Deissler, R. G.
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Role of Acoustic Streaming in Formation of Unsteady Flow in Billet Sump during Ultrasonic DC Casting of Aluminum Alloys. [PDF]
Materials (Basel), 2019 Komarov S, Yamamoto T.
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Dynamic behavior of a beam drag-force anemometer [PDF]
A cantilevered beam with strain gages attached to the fixed ends and the minimax technique were used in an experiment conducted to determine the dynamic behavior of a drag-force anemometer in high frequency, unsteady flow.
Fralick, G. C.
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Numerical and Experimental Analyses of Three- Dimensional Unsteady Flow around a Micro-Pillar Subjected to Rotational Vibration. [PDF]
Micromachines (Basel), 2018 Kaneko K +5 more
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Analysis of dynamic stall using unsteady boundary-layer theory [PDF]
The unsteady turbulent boundary layer and potential flow about a pitching airfoil are analyzed using numerical methods to determine the effect of pitch rate on the delay in forward movement of the rear flow reversal point.
Nash, J. F. +2 more
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A New Water Level Measurement Method Combining Infrared Sensors and Floats for Applications on Laboratory Scale Channel under Unsteady Flow Regime. [PDF]
Sensors (Basel), 2019 Majdalani S, Chazarin JP, Moussa R.
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